FR2961553B1 - Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur - Google Patents

Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur

Info

Publication number
FR2961553B1
FR2961553B1 FR1054849A FR1054849A FR2961553B1 FR 2961553 B1 FR2961553 B1 FR 2961553B1 FR 1054849 A FR1054849 A FR 1054849A FR 1054849 A FR1054849 A FR 1054849A FR 2961553 B1 FR2961553 B1 FR 2961553B1
Authority
FR
France
Prior art keywords
turbomachine
sector
radial
rectifier
outer shroud
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1054849A
Other languages
English (en)
French (fr)
Other versions
FR2961553A1 (fr
Inventor
Yvon Cloarec
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1054849A priority Critical patent/FR2961553B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to RU2013102305/06A priority patent/RU2587026C2/ru
Priority to RU2016102336A priority patent/RU2702204C2/ru
Priority to CA2996360A priority patent/CA2996360C/fr
Priority to CN201180040040.3A priority patent/CN103038455B/zh
Priority to BR112012032254-0A priority patent/BR112012032254B1/pt
Priority to PCT/FR2011/051372 priority patent/WO2011157956A1/fr
Priority to JP2013514770A priority patent/JP5882312B2/ja
Priority to CN201510445460.XA priority patent/CN105134304B/zh
Priority to EP11735507.3A priority patent/EP2582919B1/fr
Priority to US13/805,211 priority patent/US9228449B2/en
Priority to CA2802397A priority patent/CA2802397C/fr
Priority to EP15173476.1A priority patent/EP2949869B1/fr
Publication of FR2961553A1 publication Critical patent/FR2961553A1/fr
Application granted granted Critical
Publication of FR2961553B1 publication Critical patent/FR2961553B1/fr
Priority to JP2015201251A priority patent/JP6013576B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • F01D25/06—Antivibration arrangements for preventing blade vibration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/38—Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain position
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1054849A 2010-06-18 2010-06-18 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur Active FR2961553B1 (fr)

Priority Applications (14)

Application Number Priority Date Filing Date Title
FR1054849A FR2961553B1 (fr) 2010-06-18 2010-06-18 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
US13/805,211 US9228449B2 (en) 2010-06-18 2011-06-16 Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector
CA2996360A CA2996360C (fr) 2010-06-18 2011-06-16 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
CN201180040040.3A CN103038455B (zh) 2010-06-18 2011-06-16 用于涡轮引擎压缩机的定子角区部以及由其构成的涡轮引擎定子和包括该涡轮引擎定子的涡轮引擎
BR112012032254-0A BR112012032254B1 (pt) 2010-06-18 2011-06-16 Setor angular de estator para compressor de turbomáquina, estator de turbomáquina e turbomáquina incluindo tal estator
PCT/FR2011/051372 WO2011157956A1 (fr) 2010-06-18 2011-06-16 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
JP2013514770A JP5882312B2 (ja) 2010-06-18 2011-06-16 タービンエンジン圧縮機用のステータの角度セクタ、タービンエンジンステータ、およびそのようなセクタを含むタービンエンジン
CN201510445460.XA CN105134304B (zh) 2010-06-18 2011-06-16 用于涡轮引擎压缩机、涡轮引擎定子的定子的角区部以及包括此区部的涡轮引擎
RU2013102305/06A RU2587026C2 (ru) 2010-06-18 2011-06-16 Угловой сектор статора компрессора газотурбинного двигателя, статор газотурбинного двигателя и газотурбинный двигатель, содержащий такой сектор
RU2016102336A RU2702204C2 (ru) 2010-06-18 2011-06-16 Угловой сектор статора компрессора газотурбинного двигателя, статор газотурбинного двигателя и газотурбинный двигатель, содержащий такой сектор
CA2802397A CA2802397C (fr) 2010-06-18 2011-06-16 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
EP15173476.1A EP2949869B1 (fr) 2010-06-18 2011-06-16 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel redresseur
EP11735507.3A EP2582919B1 (fr) 2010-06-18 2011-06-16 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
JP2015201251A JP6013576B2 (ja) 2010-06-18 2015-10-09 タービンエンジン圧縮機用のステータの角度セクタ、タービンエンジンステータ、およびそのようなセクタを含むタービンエンジン

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1054849A FR2961553B1 (fr) 2010-06-18 2010-06-18 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur

Publications (2)

Publication Number Publication Date
FR2961553A1 FR2961553A1 (fr) 2011-12-23
FR2961553B1 true FR2961553B1 (fr) 2012-08-31

Family

ID=43546148

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054849A Active FR2961553B1 (fr) 2010-06-18 2010-06-18 Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur

Country Status (9)

Country Link
US (1) US9228449B2 (ja)
EP (2) EP2949869B1 (ja)
JP (2) JP5882312B2 (ja)
CN (2) CN103038455B (ja)
BR (1) BR112012032254B1 (ja)
CA (2) CA2996360C (ja)
FR (1) FR2961553B1 (ja)
RU (2) RU2702204C2 (ja)
WO (1) WO2011157956A1 (ja)

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FR2998609B1 (fr) * 2012-11-27 2018-08-10 Safran Aircraft Engines Etage redresseur de turbomachine comportant un logement et un assemblage de cordons
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FR3008455B1 (fr) * 2013-07-09 2015-08-21 Snecma Redresseur pour compresseur comportant des moyens de rattrapage de jeu
WO2016068859A1 (en) * 2014-10-28 2016-05-06 Siemens Energy, Inc. Modular turbine vane
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915370A1 (en) 2014-12-23 2016-06-23 Rolls-Royce Corporation Full hoop blade track with axially keyed features
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US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
DE102016205997A1 (de) * 2016-04-11 2017-10-12 MTU Aero Engines AG Leitschaufelsegment
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US10260527B2 (en) 2016-05-17 2019-04-16 General Electric Company Method and system for mitigating rotor bow
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track
FR3058755B1 (fr) * 2016-11-15 2020-09-25 Safran Aircraft Engines Turbine pour turbomachine
US10746047B2 (en) * 2017-10-27 2020-08-18 General Electric Company Structure for mitigating vibratory modes of counter-rotating engine rotors
CN109356660B (zh) * 2018-12-14 2021-11-19 中国航发沈阳发动机研究所 双级高压涡轮转静子组件
BE1027280B1 (fr) * 2019-05-16 2020-12-15 Safran Aero Boosters Sa Carter de compresseur pour turbomachine
FR3096734B1 (fr) * 2019-05-29 2021-12-31 Safran Aircraft Engines Ensemble pour turbomachine
FR3096731B1 (fr) * 2019-05-29 2021-05-07 Safran Aircraft Engines Ensemble pour turbomachine
WO2021167003A1 (ja) * 2020-02-20 2021-08-26 川崎重工業株式会社 ガスタービンエンジンの圧縮機の組付構造
CN111486129B (zh) * 2020-04-20 2021-05-14 中国航发湖南动力机械研究所 静子整流环结构、压气机及航空发动机
FR3111677B1 (fr) * 2020-06-23 2022-09-09 Safran Aircraft Engines Compresseur de turbomachine, procédé de montage dudit compresseur
RU2755446C1 (ru) * 2020-07-23 2021-09-16 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Спрямляющий аппарат компрессора газотурбинного двигателя
FR3119210B1 (fr) * 2021-01-27 2023-10-27 Safran Aircraft Engines Redresseur pour une turbomachine d’aéronef, une turbomachine d’aéronef equipée d’un tel redresseur.
CN114165300B (zh) * 2021-10-20 2023-06-13 中国航发四川燃气涡轮研究院 一种可降低热应力的涡轮后承力浮动结构

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Also Published As

Publication number Publication date
BR112012032254B1 (pt) 2022-09-20
US9228449B2 (en) 2016-01-05
WO2011157956A1 (fr) 2011-12-22
FR2961553A1 (fr) 2011-12-23
RU2016102336A3 (ja) 2019-08-06
CN103038455B (zh) 2015-11-25
RU2587026C2 (ru) 2016-06-10
CN105134304A (zh) 2015-12-09
CA2996360A1 (fr) 2011-12-22
BR112012032254A2 (pt) 2016-11-22
CN105134304B (zh) 2017-04-12
JP5882312B2 (ja) 2016-03-09
US20130223990A1 (en) 2013-08-29
RU2013102305A (ru) 2014-07-27
CA2802397C (fr) 2018-11-27
CN103038455A (zh) 2013-04-10
JP6013576B2 (ja) 2016-10-25
JP2016028202A (ja) 2016-02-25
EP2949869B1 (fr) 2017-03-29
EP2582919A1 (fr) 2013-04-24
RU2702204C2 (ru) 2019-10-04
EP2949869A1 (fr) 2015-12-02
CA2996360C (fr) 2019-05-21
EP2582919B1 (fr) 2015-08-05
RU2016102336A (ru) 2018-11-20
JP2013528746A (ja) 2013-07-11
CA2802397A1 (fr) 2011-12-22

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